CN205516219U - Limbs training machine - Google Patents
Limbs training machine Download PDFInfo
- Publication number
- CN205516219U CN205516219U CN201620084512.5U CN201620084512U CN205516219U CN 205516219 U CN205516219 U CN 205516219U CN 201620084512 U CN201620084512 U CN 201620084512U CN 205516219 U CN205516219 U CN 205516219U
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- CN
- China
- Prior art keywords
- crank
- hole
- carousel
- gear
- rotating disk
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Abstract
The utility model provides a limbs training machine relates to the sport equipment field, and its structure includes and counter weight box and seat is equipped with the carousel on the counter weight box, is provided with the crank on the carousel, and crank one end is provided with the clamping part, is provided with the several locating hole on the carousel, uses the carousel centre of a circle to become the round for central evenly distributed between each locating hole, crank middle part is articulated with this carousel center, still be provided with on this crank with aforementioned locating hole matched with through -hole, worn the pilot pin in the through -hole, fix crank and carousel position mutually behind the pilot pin screw in locating hole, still be provided with the steering mechanism of the clockwise or counter -clockwise turning of messenger's carousel in the weight box. The utility model discloses collect multi -functional in an organic whole, improved limbs exercise equipment's utilization ratio.
Description
Technical field
The utility model relates to sports equipment field, specifically a kind of limbs training airplane.
Background technology
It is the universal exercise apparatus in gymnasium that leg curvature machine, leg uphold machine, and this equipment can temper the muscle of human leg so that leg is stronger.Meanwhile, in order to temper the strength of upper arm, also has upper limb trainer material especially.These equipment are various in style, and expensive, but its function is the most single so that the utilization rate of every kind of equipment is the highest.
Summary of the invention
In order to solve above problem, the utility model provides a kind of limbs training airplane, gathers multi-function in integral whole, in order to improve the need of exercise of existing people.
Technical solution adopted in the utility model is:
A kind of limbs training airplane, including counterweight casing and seat, counterweight casing is provided with rotating disk, and rotating disk is provided with crank, and crank one end is provided with clamping part, rotating disk is provided with hole, several location, each location is uniformly distributed Cheng Yiquan between hole centered by the rotating disk center of circle, hinged with this center of turntable in the middle part of described crank, and this crank is additionally provided with the through hole matched with hole, aforementioned location, being installed with pilot pin in through hole, crank is fixed after screwing in hole, location by pilot pin with disk position；A steering mechanism making rotating disk clockwise or counterclockwise it is additionally provided with in ballast box.
Described limbs training airplane, its described steering mechanism includes driven gear, driving gear and the idler gear being meshed with driven gear, driving gear, described driven gear is connected to a fixed with turntable, described idler gear is provided with two groups, one of which includes a gear that can be directly meshed with driven gear, driving gear, and another group includes two gears meshed together；These two groups of idler gears change duty by reversal valve；Driving gear is connected with the pulling rope in ballast box.
Described limbs training airplane, its described clamping part is connected with crank by rotating handle, and rotating handle regulates the angle between rotating handle and crank by locking knob.
Described limbs training airplane, it is provided with the position limiting structure for preventing health from sliding at the volley on the seat.
Described limbs training airplane, its described position limiting structure includes lever.
The beneficial effects of the utility model:
Can be used for leg stretching, extension and bending weight loading exercise it can also be used to the stretching, extension of upper limbs and bending weight loading exercise；Improve training entertaining, also improve the utilization rate of limbs training equipment.
Accompanying drawing explanation
Fig. 1 is overall structure schematic diagram of the present utility model；
Fig. 2 is the structural representation of steering mechanism.
Detailed description of the invention
Below in conjunction with the accompanying drawings the utility model is described in detail below.
As shown in Figure 1, a kind of limbs training airplane, including counterweight casing 1 and seat 13, counterweight casing 1 is provided with rotating disk 6, crank 7 it is provided with on rotating disk 6, crank 7 one end is provided with clamping part 10, rotating disk 6 is provided with hole, several location 5, each location is uniformly distributed Cheng Yiquan between hole 5 centered by rotating disk 6 center of circle, in the middle part of described crank 7 hinged with this rotating disk 6 center, being additionally provided with the through hole matched with hole, aforementioned location 5 on this crank 7, be installed with pilot pin 4 in through hole, crank 7 is fixed after screwing in hole 5, location by pilot pin 4 with rotating disk 6 position.Thus can 360 degree of rotary cranks 7 be fixed in appointment position so that clamping part 10 i.e. can be used for leg exercises it can also be used to upper body exercise.
In ballast box, 1 is additionally provided with a steering mechanism 3 making rotating disk 6 clockwise or counterclockwise.By this steering mechanism 3, weight loading exercise clockwise or counterclockwise can be carried out.
Described clamping part 10 is connected with crank 7 by rotating handle 9, and rotating handle 9 regulates the angle between rotating handle 9 and crank 7 by locking knob 8.Seat 13 is provided with the lever 12 for preventing health from sliding at the volley.
As shown in Figure 2, described steering mechanism 3 includes driven gear 3-3, driving gear 3-1 and the idler gear 3-2 being meshed with driven gear 3-3, driving gear 3-1, described driven gear 3-3 is connected to a fixed with turntable 6, described idler gear 3-2 is provided with two groups, one of which includes a gear that can be directly meshed with driven gear 3-3, driving gear 3-1, and another group includes two gears meshed together；These two groups of idler gear 3-2 change duty by reversal valve；Driving gear 3-1 is connected with the pulling rope 2 in ballast box 1.Wherein the rotation direction of driving gear 3-1 is constant, is meshed with driving gear 3-1 and driven gear 3-3 respectively by different idler gear 3-2, changes direction of rotation when driven gear 3-3 bears a heavy burden.
In addition to the technical characteristic described in specification, it is the known technology of those skilled in the art.
Claims (5)
1. a limbs training airplane, including counterweight casing and seat, counterweight casing is provided with rotating disk, and rotating disk is provided with crank, crank one end is provided with clamping part, it is characterized in that, be provided with hole, several location on rotating disk, each location is uniformly distributed Cheng Yiquan between hole centered by the rotating disk center of circle, in the middle part of described crank hinged with this center of turntable, being additionally provided with the through hole matched with hole, aforementioned location on this crank, be installed with pilot pin in through hole, crank is fixed after screwing in hole, location by pilot pin with disk position；A steering mechanism making rotating disk clockwise or counterclockwise it is additionally provided with in ballast box.
Limbs training airplane the most according to claim 1, it is characterized in that, described steering mechanism includes driven gear, driving gear and the idler gear being meshed with driven gear, driving gear, described driven gear is connected to a fixed with turntable, described idler gear is provided with two groups, one of which includes a gear that can be directly meshed with driven gear, driving gear, and another group includes two gears meshed together；These two groups of idler gears change duty by reversal valve；Driving gear is connected with the pulling rope in ballast box.
Limbs training airplane the most according to claim 1, it is characterised in that described clamping part is connected with crank by rotating handle, rotating handle regulates the angle between rotating handle and crank by locking knob.
Limbs training airplane the most according to claim 1, it is characterised in that be provided with the position limiting structure for preventing health from sliding at the volley on the seat.
Limbs training airplane the most according to claim 4, it is characterised in that described position limiting structure includes lever.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620084512.5U CN205516219U (en) | 2016-01-28 | 2016-01-28 | Limbs training machine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620084512.5U CN205516219U (en) | 2016-01-28 | 2016-01-28 | Limbs training machine |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205516219U true CN205516219U (en) | 2016-08-31 |
Family
ID=56771451
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620084512.5U Expired - Fee Related CN205516219U (en) | 2016-01-28 | 2016-01-28 | Limbs training machine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205516219U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108211252A (en) * | 2018-01-10 | 2018-06-29 | 卡斯纳（苏州）医疗设备有限公司 | A kind of fracture arm strength recovery device |
| CN114534195A (en) * | 2022-03-23 | 2022-05-27 | 枣庄学院 | Be used for sports fitness to synthesize training equipment |
-
2016
- 2016-01-28 CN CN201620084512.5U patent/CN205516219U/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108211252A (en) * | 2018-01-10 | 2018-06-29 | 卡斯纳（苏州）医疗设备有限公司 | A kind of fracture arm strength recovery device |
| CN108211252B (en) * | 2018-01-10 | 2019-08-06 | 卡斯纳（苏州）医疗设备有限公司 | A kind of fracture arm strength recovery device |
| CN114534195A (en) * | 2022-03-23 | 2022-05-27 | 枣庄学院 | Be used for sports fitness to synthesize training equipment |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160831 Termination date: 20170128 |